PZL TS-11 ISKRA

 

Origin:

Poland

Type:

Two-seat military trainer

Engine:

One 2,205 lbst PZL-Rzeszow SO-3 single-shaft axial-flow turbojet

Specifications:

  • Wingspan: 10.06 m (33 ft)
  • Length: 11.15 m (36 ft 5 in)
  • Height: 3.5 m (11 ft 5½ in)
  • Wing area: 17.5 m² (188.37 sq ft)
  • Max speed at 5,000 m (16,405 ft): 720 km/h (447 mph)
  • Max cruising speed at 7,000 m (22,965 ft): 600 km/h (373 mph)
  • Range cruising speed at 7,000 m (22,965 ft): 490 km/h (304 mph)
  • Initial rate of climb: 657 m/min (2,156 ft/min)
  • Time to 6,000 m (19,685 ft): 9.6 mins
  • Service ceiling: 11,140 m (36,550 ft)
  • Range with max fuel: 1,160 km (720 miles)
  • Empty weight: 2,494 kg (5,498 lb)
  • Loaded weight: 3,810 kg (8,400 lb)

Photo source: Wikipedia

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